IIUM CubeSat Structural Subsystem Design-Reference-Cited by-同舟云学术

IIUM CubeSat Structural Subsystem Design

Published:2015-07 Issue: Volume:1115 Page:568-572
ISSN:1662-8985
Container-title:Advanced Materials Research
language:
Short-container-title:AMR

Author:

Isharuddin Siti Sarah¹,Okasha Mohamed¹,Ibrahim Sultan¹

Affiliation:

1. International Islamic University Malaysia (IIUM)

Abstract

This paper investigates the development process of a CubeSat model structure subsystem for the International Islamic University Malaysia (IIUM). Many universities around the world have participated in similar CubeSat satellite projects. CubeSat satellite enables to design and produce a fully functional satellite at low cost compared to other types of satellites. It gives the engineering students especially the aerospace one, a hands-on education, and learning about how to design their own satellite. This paper will discuss the procedures that can be used to design and test the CubeSat structure subsystem considering design goals and constraints. The analyses will consider the structure static and vibration tests utilizing ANSYS Workbench platform and SolidWorks software and the simulation results will be compared with the experimental test results on the physical model.

Publisher

Trans Tech Publications, Ltd.

Subject

General Engineering

Link

https://www.scientific.net/AMR.1115.568.pdf

Reference9 articles.

1. M. Garg, J. Sembera and M. Franki, Satellite Solutions CubeSat Design Report, University of Texas, (2003).

2. Background Paper (No. 9), Small Satellite Missions, for the Third United Nations Conference on the Exploration and Peaceful Uses of Outer Space, United Nations, Document A/COF. 184/BP/9, (1998).

3. N. Murali, A System Engineering Approach to Small Satellite Mission Formalization, Mississippi State University, (2006).

4. Rycroft and Crosby, Smaller Satellites: Bigger Business?, Spsce Studies, Vol. 6, Springer, (2002).

5. S. Haley, The Next Big Thing is Small, ASK Magazine, Issue 38, 2011. Available: http: /1. usa. gov/d8jlM4.